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GB2331180A - Magnetrons - Google Patents

Magnetrons Download PDF

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Publication number
GB2331180A
GB2331180A GB9823667A GB9823667A GB2331180A GB 2331180 A GB2331180 A GB 2331180A GB 9823667 A GB9823667 A GB 9823667A GB 9823667 A GB9823667 A GB 9823667A GB 2331180 A GB2331180 A GB 2331180A
Authority
GB
United Kingdom
Prior art keywords
anode
magnetron
vanes
anode structure
cylindrical member
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB9823667A
Other versions
GB9823667D0 (en
GB2331180B (en
Inventor
Michael Barry Clive Brady
Paul Simon Burleigh
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Teledyne UK Ltd
Original Assignee
EEV Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from GBGB9723478.5A external-priority patent/GB9723478D0/en
Application filed by EEV Ltd filed Critical EEV Ltd
Priority to GB9823667A priority Critical patent/GB2331180B/en
Publication of GB9823667D0 publication Critical patent/GB9823667D0/en
Publication of GB2331180A publication Critical patent/GB2331180A/en
Application granted granted Critical
Publication of GB2331180B publication Critical patent/GB2331180B/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J23/00Details of transit-time tubes of the types covered by group H01J25/00
    • H01J23/16Circuit elements, having distributed capacitance and inductance, structurally associated with the tube and interacting with the discharge
    • H01J23/18Resonators
    • H01J23/22Connections between resonators, e.g. strapping for connecting resonators of a magnetron
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J23/00Details of transit-time tubes of the types covered by group H01J25/00
    • H01J23/02Electrodes; Magnetic control means; Screens
    • H01J23/10Magnet systems for directing or deflecting the discharge along a desired path, e.g. a spiral path
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J23/00Details of transit-time tubes of the types covered by group H01J25/00
    • H01J23/36Coupling devices having distributed capacitance and inductance, structurally associated with the tube, for introducing or removing wave energy
    • H01J23/40Coupling devices having distributed capacitance and inductance, structurally associated with the tube, for introducing or removing wave energy to or from the interaction circuit
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J25/00Transit-time tubes, e.g. klystrons, travelling-wave tubes, magnetrons
    • H01J25/50Magnetrons, i.e. tubes with a magnet system producing an H-field crossing the E-field
    • H01J25/52Magnetrons, i.e. tubes with a magnet system producing an H-field crossing the E-field with an electron space having a shape that does not prevent any electron from moving completely around the cathode or guide electrode
    • H01J25/58Magnetrons, i.e. tubes with a magnet system producing an H-field crossing the E-field with an electron space having a shape that does not prevent any electron from moving completely around the cathode or guide electrode having a number of resonators; having a composite resonator, e.g. a helix
    • H01J25/587Multi-cavity magnetrons

Landscapes

  • Microwave Tubes (AREA)

Abstract

An anode structure for a magnetron includes anode vanes 3 having a radially extensive component 3a and a circumferentially extensive portion 3b, the cylindrical faces 3c of the circumferential portions 3b facing a cathode in the complete magnetron. The use of such vanes, which are preferably of T- or L- shape, increases inductance and hence permits low frequency radiation to be generated without increasing the dimensions of the magnetron compared to those of a conventional magnetron. Also, capacitance is increased to give a further reduction in frequency by using more than two anode straps, and preferably four anode straps 5 to 8, at each end of the anode structure. Some of the vanes may have a radially extensive component 3a only. Preferably, the anode structure is incorporated in a magnetron in which a high magnetic field of the order of 500 Gauss for a magnetron operating at 100 MHz is used. The anode shell 2 itself may form part of the magnetic return path.

Description

lWagetrons This invention relates to magnetrons and more particularly to anode structures for use in magnetrons.
Magnetrons are a well known class of microwave tube and typically comprise a central cathode surrounded by a cylindrical anode structure which defines a plurality of resonant cavities. For example, the anode structure may comprise a cylindrical anode ring within which are located a plurality of radially disposed anode vanes.
Magnetrons may be used to generate microwave radiation over a range of frequencies depending on the geometry and dimensions of the anode structure. However, magnetrons are generally considered unsuitable for use in generating low frequency radiation, for example, frequencies of 400 MHz or lower. Although these lower frequencies may be achieved by scaling up a conventional magnetron design this results in a device which occupies a large volume and is also unacceptably heavy and mechanically weak. Not only must increased amounts of materials be used to make up a larger device in any case, but also the various components must also more massive to resist mechanical stresses imposed by a larger design and to withstand the vacuum required.
The present invention seeks to provide a magnetron, and an anode structure for use in such a magneton, which is able to operate at relatively low frequencies but is also a relatively compact and low weight structure.
According to a first aspect of the invention, there is provided an anode structure for a magnetron comprising a cylindrical member having anode vanes disposed within it to define resonant cavities, each anode vane having a radially extensive portion of substantially the same thickness at the cylindrical member as the other anode vanes, and wherein each of a plurality of the anode vanes has a substantially radially extensive first portion and a second portion at its inner end which is extensive in a substantially circumferential direction.
According to a second aspect of the invention there is provided an anode structure for a magnetron comprising a cylindrical member having a plurality of anode vanes disposed within it to define resonant cavities, each anode vane disposed within the cylindrical member having a substantially radially extensive first portion and a second portion at its inner end which is extensive in a substantially circumferential direction.
According to a third aspect of the invention there in provided an anode structure for a magnetron comprising a cylindrical member having anode vanes disposed within it to define resonant cavities, wherein each anode vane of a plurality of the anode vanes has a substantially radially extensive first portion and a second portion at its inner end which is extensive in a substantially circumferential direction, and the anode vanes of the plurality being arranged alternately within the cylindrical member with anode vanes of a set of anode vanes, wherein each anode vane of the set has only a substantially radially extensive portion which is of substantially uniform thickness.
According to a fourth aspect of the invention there is provided an anode structure for a magnetron comprising a cylindrical member having anode vanes disposed within it to define resonant cavities and wherein each anode vane of a plurality of the anode vanes has a substantially radially extensive first portion and a second portion at its inner end which is extensive in a substantially circumferential direction and at one of its ends adjoins the first portion.
In a conventional magnetron, the anode vanes comprise only radially extensive portions. In an anode structure in accordance with any of the aspects of the invention, the second portion of the anode vanes effectively increases the current path length around the anode cavities, thus increasing inductance in the anode structure. As the operating frequency of the magnetron is proportional to the reciprocal of the square root of inductance multiplied by capacitance, any increase in the inductance achieved by using the invention has the effect of lowering the operating frequency of the magnetron. Thus, for a given overall diameter of the anode structure and the same number of anode cavities, a significantly lower operating frequency may be achieved by employing the invention in comparison with a conventional structure.
In one advantageous embodiment of the first and second aspects of the invention for example, the first portions of at least some of the said plurality join the respective second portions at the mid-point along the length of the second portion. This gives a "T-shape" anode vane. A T-shape configuration of anode vanes is advantageous because of the symmetry it offers. However, some aspects of the invention may be implemented using anode vanes which are an "L-shape" for example. Each of these may be arranged around the circumference of the cylindrical anode member in the same orientation or in another arrangement, the orientation of alternate L-shape anode vanes might be reversed, for example.
In a particularly advantageous embodiment of the first aspect of the invention for example, the said plurality includes all anode vanes of the anode structure. This arrangement preserves a high degree of symmetry and a relatively large increase in inductance. However, for some applications it may be desirable, for example, to alternate anode vanes having a circumferential portion with anode vanes which are of a conventional configuration, being merely radially extensive in accordance with the third aspect of the invention.
Advantageously, more than two anode straps are included at one end of the anode structure. It is further preferred that more than two anode straps are included at each end of the anode structure. Preferably, four anode straps are included at at least one end of the anode structure. In other configurations, three or more than four anode straps may be included at at least one end of the anode structure.
The use of multiple anode straps in place of the usually provided two anode straps permits a large capacitance to be achieved in the anode circuit. Capacitance exists between facing surfaces of the anode straps and by employing more than two anode straps, this capacitance may thus be increased without needing to alter the dimensions or spacing of the straps from what would normally be considered suitable. Capacitance is also added between the surfaces of the anode straps and facing surfaces of the anode vane. Thus, capacitance may be increased by increasing the facing surface areas in the anode circuit without giving rise to the difficulties in tolerancing or problems with electrical breakdown which would arise if it were attempted to move the straps closer togther to achieve an increase in capacitance.
The increase in capacitance compared to a conventional structure of the same overall dimensions gives a reduction in the magnetron operating frequency.
In one advantageous arrangement in accordance with the invention, at least one of the anode straps has a gap in its circumference located at the second portion of one of the anode vanes of the said plurality. One or more gaps may be included in an anode strap without affecting its usefulness in achieving mode separation as the greater length in the circumferential direction of the vane compared to a conventional purely radial vane permits the strap to be securely mounted in good electrical contact with the vane and also accommodate a gap. However, this leads to some reduction in capacitance and may not always be acceptable.
According to a first feature of the invention, a magnetron comprises an anode structure in accordance with either aspect of the invention and a cathode is located coaxially within the anode structure.
A magnetron in accordance with the invention may be less than one thirtieth of the weight of a scaled up conventional magnetron for operation at the same frequency. As a further comparison, the reduction in diameter achievable making use of the invention leads to an anode structure of 264 mm diameter in comparison with a diameter of 1.2 m for a conventional magnetron for operation at the same frequency of 100 MHz.
A further reduction in frequency may be achieved by providing a high magnetic field between the anode structure and the cathode. Preferably, the magnetic field strength is in the range of 500 Gauss to 2000 Gauss where the operating frequency of the magnetron is in the range of approximately 100 MHz to 400 MHz. As the operating frequency increases, an increase in magnetic field is required. As a comparison, for operation at 100 to 400 MHz, in a conventional design, it would be expected to use a magnetic field of approximately 100 Gauss to 400 Gauss.
According to a second feature of the invention, a magnetron comprises means for producing a magnetic field between the anode structure and the cathode having a field strength in the range 500 Gauss to 2000 Gauss where the operating frequency of the magnetron is in the range of 100 MHz to 400 MHz.
In a particularly advantageous embodiment in accordance with the invention, the cylindrical member of the anode structure provides a return path for the magnetic field. In one arrangement, the cylindrical member is of steel with copper coating on its inner surface.
This gives a compact structure in which it is not necessary to separately provide a magnetic return path.
Some ways in which the invention may be performed are now described by way of example with reference to the accompanying drawings, in which: Figure 1 schematically illustrates in plan view an anode structure in accordance with the invention; Figure 2 schematically shows in section along the line II-II of Figure 1 an anode vane of the anode structure of Figure 1; Figure 3 schematically shows in longitudinal section a magnetron in accordance with the present invention; and Figures 4 and 5 schematically illustrate respective different anode structures in accordance with the invention.
With reference to Figure 1, an anode structure 1 comprises a cylindrical anode shell member 2 which in this embodiment is of steel and has its interior surface coated with a thin copper layer. In other embodiments the cylindrical member 2 may be wholly of copper as in conventional magnetrons. Six anode vanes 3 are located within the cylindrical member 2.
Each vane 3 has a radially extensive portion 3a and a circumferentially extensive portion 3b at its inner end. Each anode vane 3 is thus substantially T-shaped in transverse section and presents a part-cylindrical surface 3c facing inwardly towards the region where the cathode is located in a complete magnetron. The radially extensive portions are of the same thickness il where they adjoin the cylindrical member 2. The T-shape vanes 3 present a higher inductance than would be the case with a conventional anode structure geometry in which each vane consists only of a radial component. The path for currents flowing around each anode cavity is increased as it also includes the "arms" of the T, that is, the circumferentially extensive portions 3b. Each anode vane may be a composite of two separate radial and circumferential parts which are joined or may be a single integral component.
The anode structure also includes a port 4 via which energy may be extracted during operation of the complete magnetron using conventional coupling mechanisms.
As can be more clearly seen in Figure 2, the anode structure includes four concentric anode straps 5, 6, 7 and 8 arranged coaxially within the cylindrical member 2. The straps 5 to 8 are of rectangular cross section in this embodiment but other configurations may be used if desired. The anode vane 9 shown in Figure 2 includes a cut out portion 10 in the circumferential portion 3b within which the straps 5 to 8 are located. Upstanding ridges 11 and 12 are included within the cut out portion 10 and are arranged to be in electrical contact with two of the straps 6 and 8. The other two straps 5 and 7 are not in electrical contact with anode vane 9. The bottom edge of anode vane 9 as shown also includes a cut out section 13 within which are located four additional annular anode straps 14, 15, 16 and 17. Anode straps 14 and 16 are electrically connected to anode vane 9 via ridges 18 and 19 and the other anode straps 15 and 17 are not in electrical contact. Altemate anode vanes around the cylindrical member 2 are connected in the same way as that shown in Figure 2 and the remaining anode vanes between them are connected oppositely.
Capacitance exists between facing surfaces of adjacent anode straps, being dependent on the extent of the facing area. In addition, capacitance also exists between the outermost face of the outer strap 5, say, and the facing part of anode vane 9 and similarly for the bottom outer strap 14 and the innermost faces of the two inner straps 8 and 17 which also face the anode vane 9. Capacitance also exists between the bottom face, for example, of anode strap 5 and the facing part of anode vane 9.
Because the anode straps 5 to 8 and 14 to 17 are mounted at the circumferentially extensive parts 3b of the anode vanes 3, the contribution to the capacitance which exists between them and facing parts of the anode vanes themselves is increased compared to what would be the case in a conventional design in which each anode vane has only a radial component and is of limited width.
Some of the anode straps include gaps or discontinuities in their circumference for ease of fabrication, for example, strap 5, which is electrically connected to anode vane 20 adjacent anode vane 9, has a gap 21. The circumferential portion of anode vane 20 ensures that good electrical contact for obtaining mode separation is still achievable. However, the inclusion of a gap or gaps in an anode strap does reduce capacitance and hence it may be desirable in most cases to keep the anode straps as complete annular rings to maximize capacitance.
With reference to Figure 3, a magnetron incorporating the anode structure 1 illustrated in Figure 1 and 2 also includes a cylindrical cathode 2 coaxially located within the anode structure 1 along longitudinal axis X-X through the magnetron. The magnetron includes permanent magnets 22 and 23 arranged to produce a magnetic field of relatively high strength in the gap between the cathode 2 and the anode structure 1. For example, where the magnetron is intended to operate at a frequency of 100 MHz, the magnetic field provided is approximately 500 Gauss in an axial direction in the gap. Although in this embodiment permanent magnets are included to provide the magnetic field, other means may be used. For example, an electromagnet might be employed instead. The return path of the magnetic field is provided via straps 24, through the steel cylindrical member 2 and via straps 25. The cylindrical member 2 forms part of the microwave circuit. It also defines the vacuum envelope of the magnetron and fulfils a third function of providing a magnetic return path.
The straps connecting the magnets to the cylindrical member 2 may be replaced by single components in other embodiments.
The anode structure shown in Figures 1 and 2 may of course be included in magnetrons having a conventional magnetic return path in which additional components are included and need not be used with a high magnetic field. However operating frequencies are then consequently higher.
The advantage of using the cylindrical member 2 as the magnetic return path is that it reduces the number of components required. Also, as steel is used, there is a weight saving.
If copper were to be used as in a conventional magnetron, it would need to be much thicker to withstand the stresses involved. This design also minimizes magnetic leakage to give good efficiency and increase cost effectiveness.
Figure 4 schematically illustrates another anode structure 26 having a cylindrical member 27 which contains a plurality of T-shape anode vanes 28 alternately arranged around the cylindrical member 27 with a set of anode vanes 29, these having only a radially extensive portion and no circumferential portion.
Figure 5 schematically shows yet another structure 30 having L-shape vanes 31 located within a cylindrical member 32.
Both the anode structure of Figure 4 and that of Figure 5 may be incorporated in the magnetron of Figure 3 in place of anode structure 1 or of course may be included in a conventional magnetron design in which a separate magnetic return path is included and a lower magnetic field is utilized.

Claims (18)

1. An anode structure for a magnetron comprising a cylindrical member having anode vanes disposed within it to define resonant cavities, each anode vane having a radially extensive portion of substantially the same thickness at the cylindrical member as the other anode vanes, and wherein each of a plurality of the anode vanes has a substantially radially extensive first portion and a second portion at its inner end which is extensive in a substantially circumferential direction.
2. An anode structure for a magnetron comprising a cylindrical member having a plurality of anode vanes disposed within it to define resonant cavities, each anode vane disposed within the cylindrical member having a substantially radially extensive first portion and a second portion at its inner end which is extensive in a substantially circumferential direction.
3. An anode structure for a magnetron comprising a cylindrical member having anode vanes disposed within it to define resonant cavities, wherein each anode vane of a plurality of the anode vanes has a substantially radially extensive first portion and a second portion at its inner end which is extensive in a substantially circumferential direction, and the anode vanes of the plurality being arranged alternately within the cylindrical member with anode vanes of a set of anode vanes, wherein each anode vane of the set has only a substantially radially extensive portion which is of substantially uniform thickness.
4. An anode structure for a magnetron comprising a cylindrical member having anode vanes disposed within it to define resonant cavities and wherein each anode vane of a plurality of the anode vanes has a substantially radially extensive first portion and a second portion at its inner end which is extensive in a substantially circumferential direction and at one of its ends adjoins the first portion.
5. An anode structure as claimed in claim 1, 2 or 3 wherein the first portion of at least some of the said plurality joins its respective second portion at the midpoint along the length of the second portion.
6. An anode structure as claimed in claim 1 or 4 wherein the said plurality includes all anode vanes of the anode structure.
7. An anode structure as claimed in any preceding claim wherein more than two anode straps are included at one end of the anode structure.
8. An anode structure as claimed in claim 7 wherein more than two anode straps are included at each end of the anode structure.
9. An anode structure as claimed in claim 7 or 8 wherein four anode straps are included at at least one end of the anode structure.
10. An anode structure as claimed in claim 7, 8, 9 wherein the anode straps are connected to second portions of the said plurality of anode vanes.
II. An anode structure as claimed in claim 10 wherein at least one of the anode straps has a gap in its circumference located at the second portion of one of the anode vanes of the said plurality.
12. A magnetron comprising an anode structure as claimed in any preceding claim and a cathode located coaxially within it.
13. A magnetron as claimed in claim 12 comprising means for producing a magnetic field between the anode structure and the cathode having a field strength in the range 500 Gauss to 2000 Gauss where the operating frequency of the magnetron is in the range of 100 MHz to 400 MHz.
14. A magnetron as claimed in claim 12 or 13 wherein the cylindrical member ofthe anode structure provides a return path for the magnetic field.
15. A magnetron as claimed in claim 14 wherein the cylindrical member is of steel with a copper layer on its inner surface.
16. A magnetron comprising means for producing a magnetic field between the anode structure and the cathode having a field strength in the range 500 Gauss to 2000 Gauss where the operating frequency of the magnetron is in the range of 100 MHz to 400 MHz.
17. An anode structure substantially as illustrated in and described with reference to the accompanying drawings.
18. A magnetron substantially as illustrated in and described with reference to Figure 3 of the accompanying drawings.
GB9823667A 1997-11-07 1998-10-30 Magnetrons Expired - Lifetime GB2331180B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9823667A GB2331180B (en) 1997-11-07 1998-10-30 Magnetrons

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB9723478.5A GB9723478D0 (en) 1997-11-07 1997-11-07 Magnetrons
GB9823667A GB2331180B (en) 1997-11-07 1998-10-30 Magnetrons

Publications (3)

Publication Number Publication Date
GB9823667D0 GB9823667D0 (en) 1998-12-23
GB2331180A true GB2331180A (en) 1999-05-12
GB2331180B GB2331180B (en) 2002-02-27

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Family Applications (1)

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GB9823667A Expired - Lifetime GB2331180B (en) 1997-11-07 1998-10-30 Magnetrons

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Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB740182A (en) * 1953-01-09 1955-11-09 British Thomson Houston Co Ltd Improvements relating to the production of shaped metal bodies having internal cavities, such as magnetron anodes
GB806551A (en) * 1955-07-04 1958-12-31 Philips Electrical Ind Ltd Improvements in or relating to magnetrons
GB921356A (en) * 1958-04-22 1963-03-20 Arnoux Corp Improvements in or relating to magnetron oscillators
EP0519803A1 (en) * 1991-06-21 1992-12-23 Thomson Tubes Electroniques Strapped magnetron with frequency stabilisation

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62216134A (en) * 1986-03-17 1987-09-22 Hitachi Ltd Anode structure of magnetron
JPH0521014A (en) * 1991-07-17 1993-01-29 Hitachi Ltd Magnetron
JPH0817354A (en) * 1994-06-28 1996-01-19 Toshiba Hokuto Denshi Kk Anode structure of magnetron

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB740182A (en) * 1953-01-09 1955-11-09 British Thomson Houston Co Ltd Improvements relating to the production of shaped metal bodies having internal cavities, such as magnetron anodes
GB806551A (en) * 1955-07-04 1958-12-31 Philips Electrical Ind Ltd Improvements in or relating to magnetrons
GB921356A (en) * 1958-04-22 1963-03-20 Arnoux Corp Improvements in or relating to magnetron oscillators
EP0519803A1 (en) * 1991-06-21 1992-12-23 Thomson Tubes Electroniques Strapped magnetron with frequency stabilisation

Also Published As

Publication number Publication date
GB9823667D0 (en) 1998-12-23
GB2331180B (en) 2002-02-27

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PE20 Patent expired after termination of 20 years

Expiry date: 20181029